Accession Number : ADB063024

Title :   Spin Coupled Accelerometer Gyro (SCAG).

Descriptive Note : Final rept. Aug 77-Aug 81,

Corporate Author : TELEDYNE SYSTEMS CO NORTHRIDGE CA

Report Date : DEC 1981

Pagination or Media Count : 270

Abstract : The Program demonstrated the technical feasibility of dry-tuned sensor technology to the development of a four-axis multifunction sensor capable of providing two outputs proportional to linear acceleration and two outputs proportional to angular rate. The performance levels of the gyro and accelerometer outputs are consistent with requirements of a range of tactical applications.

Descriptors :   *GYROSCOPES, *ACCELEROMETERS, *INERTIAL NAVIGATION, *GUIDED MISSILE COMPONENTS, COUPLING(INTERACTION), SPINNING(MOTION), SUSPENSION DEVICES, HINGES, WEIGHT, COST EFFECTIVENESS, DEGREES OF FREEDOM, RELIABILITY, CIRCUIT ANALYSIS, SCHEMATIC DIAGRAMS.

Subject Categories : Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE